Author Topic: SpaceX F9 : Starlink group 6-1 : CCSFS SLC-40 : 27 February 2023 (23:13 UTC)  (Read 49271 times)

Offline weepingdragon

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starlink 6-01 v2-mini top down view screencaps from 1080p webcast

 :o brain bent trying figure out what expected of tension rod with normal 2nd stage fairing view, then WONDER of CAM on TOP of the stick!!!   ;D :-*

Offline weepingdragon

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should've known to check the boss man's twitter feed for great clip 1st  :)

https://twitter.com/i/status/1630346730402205696

Offline wannamoonbase

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Love the stack to camera. 

I want to see that during deployment
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!


Offline matthewkantar

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Wow! Took a second to figure out what I was looking at. Looks like no more free flying tension rods, deployment system will reenter with stage?

Offline kevin-rf

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Wonder if the tension rods have some sort of post deployment locking mechanism to prevent them flopping around during the deorbit burn.
If you're happy and you know it,
It's your med's!

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twitter.com/planet4589/status/1630455524666867712

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First few SupTLE orbit datasets are in for Starlink Group 6-1 and it's very ineresting: as expected the deploy orbit is 365 x 372 km x 43.0 deg, so same inclination as Group 5; but the satellite *names* are a new sequence:

https://twitter.com/planet4589/status/1630455878921994240

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Existing Starlinks had names up to Starlink-5800 or so; these ones are in the Starlink-30000 series  (2023-026A is Starlink 30050). This will make it easy to distinguish the V2Minis from the V1.5 sats

Online FutureSpaceTourist

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https://twitter.com/13ericralph31/status/1630435132808237056

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Love the janky-but-it-works vibes from the new Starlink V2 Mini deployment mechanism lol. Starlink V2 launches will no longer create guaranteed debris (however short-lived) in the form of tensioning rods, as they will now reenter with the Falcon upper stage!

twitter.com/13ericralph31/status/1630435370193293314

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For example, I think this block on the crossbeam is aluminum honeycomb that's meant to crush against the upper stage to prevent the rod assembly from bouncing back up! Falcon booster legs have a similar 'crush cores' that act like single-use suspension during hard landings.

https://twitter.com/13ericralph31/status/1630438575321022466

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Also the supersized zip ties holding the wire harness to the rod, probably for the camera at the top! If it works, it works 😂

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Ltwitter.com/tskelso/status/1630500476310659072

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CelesTrak has ephemeris-based SupGP data for all 21 v2 mini satellites from the #Starlink Group 6-1 launch (2023-026) from Cape Canaveral on Feb 27 at 23:13:50 UTC: spaceflightnow.com/2023/02/27/fal…. The latest data for that launch can be found at: https://celestrak.org/NORAD/elements/supplemental/table.php?INTDES=2023-026

https://twitter.com/tskelso/status/1630504126261129217

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A quick visual check of the pre-launch & ephemeris-based SupGP data for #Starlink Group 6-1 shows the single-satellite (72001) in the pack of the ephemeris-based results, with the stack (72000) not far behind, confirming the drag modeling for the v2 minis.

Offline scr00chy

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What altitude will these sats be operated at? I thought 530 km because that's what the FCC license has for Gen2 sats with 43° inclination, but Jonathan McDowell seems to have the first 21 sats listed at some Group 5 subshells with altitudes of 553 and 559 km: https://planet4589.org/space/con/conlist.html

Also, how does this work together with the Starlink 5-X missions which are also deployed to 43°? I'm very confused with the nomenclature and constellation configuration...

Offline OceanCat

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It looks like they exercised freedom to move shells. From the authorization:

Quote
80. Orbital Tolerances. The satellites authorized in this grant are planned for operations in
orbital shells centered at altitudes from 525 km to 535 km. SpaceX has requested orbital tolerances of
+70 km and -50 km, i.e., the satellites in any orbital shell can be maintained for regular operations
anywhere within an altitude range of 70 kilometers above or 50 kilometers below the center altitude...

82. The record does not reflect with any specificity a need for Gen2 Starlink satellite
operations at altitudes above 580 km, as opposed to the +45 to +55 km tolerance that can be achieved if
operations are maintained below 580 km. We also note that one of the reasons for larger orbital
tolerances that SpaceX identifies—effects of solar radiation on the orbits of spacecraft—is less
pronounced for the particular orbital shells authorized by this grant than for lower altitudes. We will
follow the approach of the SpaceX Third Modification Order, and require SpaceX to restrict its Gen2
Starlink operations to below 580 km.

The satellites at 553 km looks like drifting to their final spots at 559 km. They all arrived at 553 km first, now the majority moved to 559 km.

Offline jacqmans

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One I took from the beach...

Online FutureSpaceTourist

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Offline scr00chy

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It looks like they exercised freedom to move shells. From the authorization:

Quote
80. Orbital Tolerances. The satellites authorized in this grant are planned for operations in
orbital shells centered at altitudes from 525 km to 535 km. SpaceX has requested orbital tolerances of
+70 km and -50 km, i.e., the satellites in any orbital shell can be maintained for regular operations
anywhere within an altitude range of 70 kilometers above or 50 kilometers below the center altitude...

82. The record does not reflect with any specificity a need for Gen2 Starlink satellite
operations at altitudes above 580 km, as opposed to the +45 to +55 km tolerance that can be achieved if
operations are maintained below 580 km. We also note that one of the reasons for larger orbital
tolerances that SpaceX identifies—effects of solar radiation on the orbits of spacecraft—is less
pronounced for the particular orbital shells authorized by this grant than for lower altitudes. We will
follow the approach of the SpaceX Third Modification Order, and require SpaceX to restrict its Gen2
Starlink operations to below 580 km.

The satellites at 553 km looks like drifting to their final spots at 559 km. They all arrived at 553 km first, now the majority moved to 559 km.

So basically any of the authorized Gen2 sats can be operated anywhere between 475 and 580 km?

Offline r1279

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The satellites at 553 km looks like drifting to their final spots at 559 km. They all arrived at 553 km first, now the majority moved to 559 km.

Are we sure it's final?  I'm not an expert in orbital mechanics but wondered if these G5-1 sats were at a higher altitude so the gap to the drifting/raising groups of G5-2, G5-3,... sats closes faster [getting the first planes into position faster]
« Last Edit: 02/28/2023 06:40 pm by r1279 »

Offline vaporcobra

It looks like they exercised freedom to move shells. From the authorization:

Quote
80. Orbital Tolerances. The satellites authorized in this grant are planned for operations in
orbital shells centered at altitudes from 525 km to 535 km. SpaceX has requested orbital tolerances of
+70 km and -50 km, i.e., the satellites in any orbital shell can be maintained for regular operations
anywhere within an altitude range of 70 kilometers above or 50 kilometers below the center altitude...

82. The record does not reflect with any specificity a need for Gen2 Starlink satellite
operations at altitudes above 580 km, as opposed to the +45 to +55 km tolerance that can be achieved if
operations are maintained below 580 km. We also note that one of the reasons for larger orbital
tolerances that SpaceX identifies—effects of solar radiation on the orbits of spacecraft—is less
pronounced for the particular orbital shells authorized by this grant than for lower altitudes. We will
follow the approach of the SpaceX Third Modification Order, and require SpaceX to restrict its Gen2
Starlink operations to below 580 km.

The satellites at 553 km looks like drifting to their final spots at 559 km. They all arrived at 553 km first, now the majority moved to 559 km.

So basically any of the authorized Gen2 sats can be operated anywhere between 475 and 580 km?

Correct!

Offline billh

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The launch caused quite a stir in the Virgin Islands. My son lives on St. Croix and he sent me this picture from social media. There was also this article:
https://viconsortium.com/vi-technology/virgin-islands-not-aliens-just-satellites-spacex-launch-on-monday-night-lights-up-skies-in-the-northern-caribbean

Online FutureSpaceTourist

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https://twitter.com/spaceoffshore/status/1631282683111243776

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Doug arrived at Port Canaveral last night with both fairing halves from Starlink 6-1 on board.

Unloading now live here: nsf.live/spacecoast

Online FutureSpaceTourist

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https://twitter.com/jerrypikephoto/status/1631323293348143107

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Welcome back B1076.3! Falcon 9 returns to Port Canaveral, after delivering the first batch of Starlink V2 mini satellites

Online FutureSpaceTourist

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https://twitter.com/tgmetsfan98/status/1631329924081491968

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B1076 is back at Port Canaveral aboard A Shortfall of Gravitas, returned from the Starlink Group 6-1 mission!

nsf.live/spacecoast

 

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